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DG Flugzeugbau DG-1000T にも： 修理マニュアル (16 ページ)
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Maintenance Manual DG-1000T
1.12.6 Starter:
Electric starter motor, type see section 8.1.
1.12.7 Ignition system:
a)
spark plugs;
Electrode gap 0.5 mm (0.02 in.), type see section 8.1.
b)
Ignition coils: One coil per cylinder, type see section 8.1
1.12.8 Throttle cable connections
The cables can be finely adjusted at the adjusting screws located at the intake
manifolds (holders for the Bowden outers).
The cables are 1.5 mm diameter Bowden-cable
The stop for idle adjustment is at the rear carburettor.
Friction brake for throttle control: This device is located at the control bellcrank
in the instrument panel.
The brake force must be adjusted for a control force of 15 - 50 N
(3 - 11 lbs.).
Option: throttle handle in rear cockpit TN1000/15:
a) No friction brake installed.
b) The interconnection between front and rear throttle handles is by means of
2 hydraulic cylinders and hydraulic lines.
Periodical service is not required. Instructions for service and repair are given
in enclosure 3 for this MM.
1.12.9 Propeller stopper
Automatic operation: During powerplant retraction the propeller stopper is
moved forward in the propeller circle by a gas strut (with compensator spring).
Issued: March 2008
TN 1000/15
2 Inspections
2.1 Daily inspection
see flight manual section 4.3
2.2 Regular inspections
A After 200 flight hours and during the annual inspection
Check the rudder cables for wear especially around the S tubes on the rudder
pedals. Worn rudder cables should be replaced (see section 4.2). Check the
sealing of the rudder (see section 1.3.5).
B Annual inspection (and 100hr inspection – only for USA)
•
Execute all items of the daily inspection see flight manual section 4.3.
•
Inspect all bolted connections and locking devices ie. locknuts, split pins
etc.
•
Check all metal parts for adequate greasing and rust prevention. (see
section 3.3).
•
Check the control surface deflections (see sections 1.2 up to 1.4).
•
Check the free play in all control circuits (see section 1.2 up to 1.6)
•
Check the fore and aft play of the wings (see section 1.11).
•
Check the canopy emergency releases according to section 7.14 of the
flight manual.
•
Check the rubber cords in the control system (see sections 1.2.6 and
1.7.5.
•
Check the thickness of the wheel brake linings (see section 1.6.4).
•
Check if the brake fluid has to be exchanged (see section 1.6.4).
•
Check the airbrakes according to section 4.4.
•
Check the fin ballast tank system according to section 1.8.2.2.
•
Check if the powerplant has been serviced according to section 3.6.1.
•
Check the friction brake of the throttle control (see section 1.12.8).
Option: throttle handle in rear cockpit TN1000/15:
Check of friction brake not applicable, not installed.
•
Check the torque of the propeller bolts (see section 3.6.1 item 23).
•
Tow hooks: The operating and maintenance instructions for the release
mechanisms, see sect. 0.4.4 of this maintenance manual have to be
followed.
•
All-up weight and centre of gravity: These should be checked at least
every 4 years during the yearly inspection.
1.19
Issued March 2008
Maintenance Manual DG-1000T
TN 1000/15
2.1